Could someone supply me with the length of the leading edge foam cores  at the spar?


Length of the inboard foam core a the spar 'tip rib to the fuselage inboard side'?

Length of the outboard foam core at the spar 'outboard side of the fuselage to the tip rib'?

Clayton trimmed the stock cores.  Which one or both & by how much is the question?

Thank You 
JEC

David ,

Thank You!   

That post does seem to answer my quandary.  I understood the asymmetry, but could not quite understand how it was done.

I had read the post before but not close enough, nor pondered over it.  I now see that it does have the exact answer to my question.

I am sure Mike's numbers are right now that I have looked at it closely. As when the leading edge numbers are added + the fuselage they equal something close to 48", the length of a spruce spar.  I kept coming up 48"+

Thank you again.